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A330/A340 FLEET PER-CRZ-AEO-ICQ-70 P 10/12
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A330/A340 FLEET PER-CRZ-AEO-ICQ-70 P 11/12
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A330/A340 FLEET PER-CRZ-AEO-ICQ-70 P 12/12
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A330/A340 FLEET PER-CRZ-OEI-GEN-05 P 1/4
FCOM 19 AUG 10
GENERAL
INTRODUCTION
Applicable to:
This chapter provides the one engine out performance data to be used for the conduct and
monitoring of the flight following an engine failure.
The diversion strategy (descent and cruise speed schedules) shall be selected, and specified in the
operator’s routes specifications, as a function of the prevailing operational factors (e.g. obstacles
clearance requirements).
INTRODUCTION
Applicable to: ,
This chapter provides the single engine out performance data to be used for the conduct and
monitoring of the flight following an engine failure.
The diversion strategy (descent and cruise speed schedules) shall be selected, and specified in the
operator’s routes specifications, as a function of the prevailing operational factors (e.g. obstacles
clearance requirements and/or ETOPS operation).
FLIGHT PREPARATION
Applicable to:
In readiness for a possible engine failure occurring during the flight, any flight shall be planned so as
to comply with any of the following requirements, as applicable :
• obstacle clearance,
• oxygen.
FLIGHT PREPARATION
Applicable to: ,
In readiness for a possible engine failure occurring during the flight, any flight shall be planned so as
to comply with any of the following requirements, as applicable :
• obstacle clearance,
• oxygen,
• maximum diversion distance (ETOPS operation).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A330/A340 FLEET PER-CRZ-OEI-GEN-05 P 2/4
FCOM 19 AUG 10
The following FCOM sections provide flight preparation and fuel planning information :
• Refer to PER-FPL-GEN-INT INTRODUCTION, for Standard Fuel Planning,
• REFER TO PRO SPO 40A 10 GEN, for Extended Range Operation (ETOPS) and associated fuel
requirements.
STRATEGY
Applicable to:
In most cases, no constraining obstacle will be found on the route and the standard strategy will be
adopted :
descent at M .82/300 ‐ kt, maximum continuous thrust.
‐ cruise close to LRC ceiling (optimum altitude).
‐ descent to destination at 300 kt/250 kt, idle thrust.
If constraining obstacles are on the route, the obstacle strategy will be adopted :
‐ descent then cruise at green dot speed, maximum continuous thrust.
‐ as soon as obstacles are cleared, reversion to standard strategy.
The in cruise check tables show the fuel and the time required to cover a given air distance from any
moment in cruise to landing.
The tables are established for :
‐ Long range speed
‐ Descent at M .82/300 kt/250 kt
‐ Approach and Landing (330 kg or 720 lb - 6 min IFR)
‐ ISA conditions
‐ A CG of 30 %
‐ Pack flow LO
‐ Anti ice OFF
Note: Approximate increase in fuel consumption compared to all engine operative.
≤􀀃M􀀃.82􀀃or􀀃LRC􀀃M􀀃.83􀀃M􀀃.84􀀃
Add +15 % +10 % –
STRATEGY
Applicable to: ,
Depending on the prevailing operational constraints, the most appropriate diversion strategy shall be
selected, out of the following options :
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A330/A340 FLEET PER-CRZ-OEI-GEN-05 P 3/4
FCOM 19 AUG 10
STANDARD FIXED SPEED STRATEGIES
STRATEGY OBSTACLE STRATEGY 310 kt VMO
DESCENT
TO CEILING • M .82/300 kt
• MCT
• Green Dot Speed
• MCT
• M .82/310 kt
• MCT
• M .82/330 kt
• MCT
CRUISE LR ceiling
LR speed
‐ Obstacle not cleared:
Maintain Green Dot
Speed at MCT
‐ Obstacle cleared :
Revert to standard
strategy
FL per Refer to
PRO-SPO-40A-60
ETOPS FUEL
FROM CRITICAL
POINT TO
LANDING ONE
ENGINE-OUT
CRUISE AT
310KTMCT/310 kt
FL per Refer to
PRO-SPO-40A-60
ETOPS FUEL FROM
　
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